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Overview of high performance aircraft propulsion researchThe overall scope of the NASA Lewis High Performance Aircraft Propulsion Research Program is presented. High performance fighter aircraft of interest include supersonic flights with such capabilities as short take off and vertical landing (STOVL) and/or high maneuverability. The NASA Lewis effort involving STOVL propulsion systems is focused primarily on component-level experimental and analytical research. The high-maneuverability portion of this effort, called the High Alpha Technology Program (HATP), is part of a cooperative program among NASA's Lewis, Langley, Ames, and Dryden facilities. The overall objective of the NASA Inlet Experiments portion of the HATP, which NASA Lewis leads, is to develop and enhance inlet technology that will ensure high performance and stability of the propulsion system during aircraft maneuvers at high angles of attack. To accomplish this objective, both wind-tunnel and flight experiments are used to obtain steady-state and dynamic data, and computational fluid dynamics (CFD) codes are used for analyses. This overview of the High Performance Aircraft Propulsion Research Program includes a sampling of the results obtained thus far and plans for the future.
Document ID
19940035346
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Biesiadny, Thomas J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 16, 2013
Publication Date
October 1, 1992
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
SAE PAPER 921983
Report Number: SAE PAPER 921983
Meeting Information
Meeting: SAE, Aerotech ''92 Conference
Location: Anaheim, CA
Country: United States
Start Date: October 5, 1992
End Date: October 8, 1992
Sponsors: SAE
Accession Number
94A12001
Funding Number(s)
PROJECT: RTOP 505-68-32
Distribution Limits
Public
Copyright
Other

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